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首页> 外文期刊>Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow >Temporally optimized spanwise vorticity sensor measurements in turbulent boundary layers
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Temporally optimized spanwise vorticity sensor measurements in turbulent boundary layers

机译:在湍流边界层中临时优化的翼展方向涡度传感器测量

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摘要

Multi-element hot-wire anemometry was used to measure spanwise vorticity fluctuations in turbulent boundary layers. Smooth wall boundary layer profiles, with very good spatial and temporal resolution, were acquired over a Karman number range of 2000-12,700 at the Melbourne Wind Tunnel at the University of Melbourne and the University of New Hampshire's Flow Physics Facility. A custom hot-wire probe was necessary to simultaneously obtain velocity and spanwise vorticity measurements centered at a fixed point in space. A custom calibration/processing scheme was developed to utilize single-wall-parallel wires to optimize the accuracy of the measured wall-normal velocity fluctuations derived from the sensor's x-array.
机译:使用多元素热线风速仪测量湍流边界层中翼展方向的涡度波动。在墨尔本大学和新罕布什尔大学的流动物理设施的墨尔本风洞中,在2000-12700的卡曼数范围内获得了具有很好的时空分辨率的光滑壁边界层剖面。必须同时使用定制的热线探针,以同时获得以空间中的固定点为中心的速度和翼展方向涡度测量结果。开发了一种定制的校准/处理方案,以利用单壁平行线来优化从传感器的x阵列得出的所测壁法向速度波动的准确性。

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